JPH0641278B2 - 航空機の操縦空力面設定装置 - Google Patents
航空機の操縦空力面設定装置Info
- Publication number
- JPH0641278B2 JPH0641278B2 JP57053646A JP5364682A JPH0641278B2 JP H0641278 B2 JPH0641278 B2 JP H0641278B2 JP 57053646 A JP57053646 A JP 57053646A JP 5364682 A JP5364682 A JP 5364682A JP H0641278 B2 JPH0641278 B2 JP H0641278B2
- Authority
- JP
- Japan
- Prior art keywords
- signal
- airspeed
- attitude
- circuit
- pitch
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 230000004044 response Effects 0.000 claims description 19
- 230000008859 change Effects 0.000 claims description 12
- 230000001360 synchronised effect Effects 0.000 claims description 3
- 239000004020 conductor Substances 0.000 description 128
- 230000006870 function Effects 0.000 description 27
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 description 21
- 230000007704 transition Effects 0.000 description 10
- 125000004122 cyclic group Chemical group 0.000 description 8
- 230000007246 mechanism Effects 0.000 description 7
- 230000007423 decrease Effects 0.000 description 6
- 230000010354 integration Effects 0.000 description 6
- 230000008878 coupling Effects 0.000 description 5
- 238000010168 coupling process Methods 0.000 description 5
- 238000005859 coupling reaction Methods 0.000 description 5
- 239000003990 capacitor Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000009966 trimming Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000008034 disappearance Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000002441 reversible effect Effects 0.000 description 3
- 229920006395 saturated elastomer Polymers 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 230000009471 action Effects 0.000 description 2
- 238000007792 addition Methods 0.000 description 2
- 230000000903 blocking effect Effects 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- WABPQHHGFIMREM-IGMARMGPSA-N lead-207 Chemical compound [207Pb] WABPQHHGFIMREM-IGMARMGPSA-N 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- 230000003213 activating effect Effects 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 210000003811 finger Anatomy 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000005226 mechanical processes and functions Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 210000003813 thumb Anatomy 0.000 description 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
- B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US248768 | 1981-03-30 | ||
| US06/248,768 US4477876A (en) | 1981-03-30 | 1981-03-30 | Dual response aircraft reference synchronization |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5861098A JPS5861098A (ja) | 1983-04-11 |
| JPH0641278B2 true JPH0641278B2 (ja) | 1994-06-01 |
Family
ID=22940600
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP57053646A Expired - Lifetime JPH0641278B2 (ja) | 1981-03-30 | 1982-03-30 | 航空機の操縦空力面設定装置 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4477876A (enrdf_load_stackoverflow) |
| JP (1) | JPH0641278B2 (enrdf_load_stackoverflow) |
| BR (1) | BR8201660A (enrdf_load_stackoverflow) |
| DE (1) | DE3210817A1 (enrdf_load_stackoverflow) |
| GB (1) | GB2095868B (enrdf_load_stackoverflow) |
| IT (1) | IT1151380B (enrdf_load_stackoverflow) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5213283A (en) * | 1991-08-28 | 1993-05-25 | United Technologies Corporation | Low speed turn coordination for rotary wing aircraft |
| US5222691A (en) * | 1991-08-28 | 1993-06-29 | United Technologies Corporation | Automatic turn coordination trim control for rotary wing aircraft |
| US5178307A (en) * | 1991-08-28 | 1993-01-12 | United Technologies Corporation | High speed yaw control system for rotary wing aircraft |
| US5169090A (en) * | 1991-08-28 | 1992-12-08 | United Technologies Corporation | Attitude synchronization for model following control systems |
| US5238203A (en) * | 1991-08-28 | 1993-08-24 | United Technologies Corporation | High speed turn coordination for rotary wing aircraft |
| FR2741855B1 (fr) * | 1995-12-05 | 1998-01-30 | Eurocopter France | Systeme de manche cyclique assurant la stabilite en vitesse d'un helicoptere |
| US9157415B1 (en) * | 2014-03-21 | 2015-10-13 | General Electric Company | System and method of controlling an electronic component of a wind turbine using contingency communications |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3128968A (en) * | 1964-04-14 | Aircraft control servo apparatus having signal memorizing means | ||
| US2594326A (en) * | 1947-12-31 | 1952-04-29 | Bendix Aviat Corp | Trim tab servomotor control |
| US3062486A (en) * | 1958-11-19 | 1962-11-06 | Honeywell Regulator Co | Control system |
| US3275269A (en) * | 1963-10-23 | 1966-09-27 | Sperry Rand Corp | Dual period aircraft control system |
| US3578268A (en) * | 1969-01-21 | 1971-05-11 | Lear Siegler Inc | Automatic pitch control system |
| US3578269A (en) * | 1969-06-11 | 1971-05-11 | Lear Siegler Inc | Automatic flare and altitude hold system |
| US4129275A (en) * | 1974-11-22 | 1978-12-12 | The Boeing Company | Automatic flight control apparatus for aircraft |
| US4078749A (en) * | 1977-05-24 | 1978-03-14 | United Technologies Corporation | Helicopter stick force augmentation null offset compensation |
| US4281811A (en) * | 1979-06-15 | 1981-08-04 | Edo-Aire Mitchell | Pitch trim system for aircraft |
| US4382283A (en) * | 1980-08-08 | 1983-05-03 | United Technologies Corporation | Helicopter attitude and airspeed acquisition and retention system |
-
1981
- 1981-03-30 US US06/248,768 patent/US4477876A/en not_active Expired - Lifetime
-
1982
- 1982-03-05 GB GB8206533A patent/GB2095868B/en not_active Expired
- 1982-03-24 DE DE19823210817 patent/DE3210817A1/de active Granted
- 1982-03-24 BR BR8201660A patent/BR8201660A/pt not_active IP Right Cessation
- 1982-03-30 IT IT20488/82A patent/IT1151380B/it active
- 1982-03-30 JP JP57053646A patent/JPH0641278B2/ja not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| BR8201660A (pt) | 1983-02-16 |
| GB2095868A (en) | 1982-10-06 |
| DE3210817C2 (enrdf_load_stackoverflow) | 1992-02-06 |
| DE3210817A1 (de) | 1982-10-21 |
| GB2095868B (en) | 1984-08-30 |
| US4477876A (en) | 1984-10-16 |
| IT1151380B (it) | 1986-12-17 |
| IT8220488A0 (it) | 1982-03-30 |
| JPS5861098A (ja) | 1983-04-11 |
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